THERMAL EFFECTS OF SHOCKWAVE TURBULENT BOUNDARY LAYER INTERACTION AT MACH NUMBERS 3 AND 5

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Document Details

Document Type
Technical Report
Publication Date
Nov 12, 1962
Accession Number
AD0298671

Entities

People

  • T. J. Fabish
  • V. Levin

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Data Reduction
  • Flow Fields
  • Fluid Dynamics
  • Free Stream
  • Heat Transfer
  • Heat Transfer Coefficients
  • Instrumentation
  • Mach Number
  • Pressure Distribution
  • Pressure Gradients
  • Pressure Measurement
  • Test Facilities
  • Turbulent Boundary Layer
  • Turbulent Flow
  • Two Dimensional
  • Wind Tunnels